发明名称 Flowsleeve of a turbomachine component
摘要 A flowsleeve of a turbomachine component includes an annular body (30) including an upstream casing (321) and a downstream casing (322). The upstream casing defines a fuel feed (70), and the downstream casing defines an airway opening (80), and a premixing passage (90). The premixing passage (90) is fluidly coupled to the fuel feed (70) and the airway opening (80) and has a passage interior in which fuel and air receivable from the fuel feed and the airway opening, respectively, are combinable to form a fuel and air mixture.
申请公布号 EP2613091(A2) 申请公布日期 2013.07.10
申请号 EP20120198319 申请日期 2012.12.20
申请人 GENERAL ELECTRIC COMPANY 发明人 STOIA, LUCAS JOHN;DEFOREST, RUSSELL PIERSON;MELTON, PATRICK BENEDICT
分类号 F23R3/28;F23R3/34;F23R3/54 主分类号 F23R3/28
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